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Emergency and rescue aircraft

a technology for emergency rescue and aircraft, applied in the field of aeronautical engineering, can solve the problems of not being able to adapt to rough platforms, water and launches, and the decision on a prototype cannot be used for carrying out wrecking,

Inactive Publication Date: 2012-05-15
KHAKIMOV BORIS V +3
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Benefits of technology

The design achieves fast ascent and high-speed flight, safe mooring and landing on various surfaces, efficient rescue operations, and prolonged monitoring capabilities, ensuring stability and safety through controlled center of gravity and metacentric height, allowing operation in challenging environments like mountains and high-rise structures.

Problems solved by technology

The technical decision on a prototype cannot be used for carrying out of wrecking, including is not adapted for mooring for objects at height and people evacuation from the top floors of buildings, and also is not adapted for landing to rough platforms, to water and launches from them.

Method used

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  • Emergency and rescue aircraft
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Examples

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Embodiment Construction

[0030]The survival aircraft (FIG. 1,) consists of the case, for example, a fuselage 1, lifting surfaces, for example, the wings 2 located in the same plane with the bottom part of a fuselage, 1 fin 3, the aerodynamic modules 4 containing engines and propulsion devices, (on FIGS. are not shown). Configuration of aerodynamic modules 4 is as toroidal rotation bodies which cross-section section in a plane which are passing through their rotation axis has an aerodynamic profile 5. Aerodynamic modules 4 can turn from a vertical direction of draft force on the horizontal. (FIG. 4). The device contains maneuverable propulsion devices 6. The main fuselage volume is occupied with envelopes 7 (FIGS. 1, 2), filled with lifting gas (helium). On the hole length of the bottom fuselage part there is a pass through 8 (FIG. 2) having a function of force beam, also it is the additional bearing device executed in the form of lifting designs. Pass through connects the crew cabin 9 located in a nose fuse...

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PUM

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Abstract

A rescue aircraft having a rigid body with gas-filled envelopes and propulsion devices located inside rotatable aerodynamic toroidal modules. A longitudinal through passage in the lower part of the aircraft connects a crew cabin, a cargo-and-passenger compartment, fuel tanks, and accessories. The aircraft has exit hatches, mooring devices, and a gangway with railings and a removable cart. The aircraft also has a cross passage with exits onto its wings and a vertical passage with a pulley and other devices for lowering and lifting people and cargo. The lower part of the aircraft and hollow wings are filled with a foamed plastic for buoyancy and strength.

Description

RELATED APPLICATIONS[0001]This application is a Continuation of International Application No. PCT / RU2008 / 000068, filed on Feb. 5, 2008, which claims priority to Russian Patent Application No. 2007104241, filed on Feb. 5, 2007, both of which are incorporated herein by reference in their entirety.FIELD OF THE INVENTION[0002]The invention concerns area of aeronautical engineering, namely to designs of the multipurpose combined aircrafts. This invention can be used as emergency evacuation equipment for people from high-rise buildings, saving equipment of people in mountains, on water, equipment for liquidation of failures and fire extinguishing, equipment for monitoring of highways and territories, as an assembly and cargo-passenger transport vehicle.BACKGROUND OF THE INVENTION[0003]The multipurpose combined aircrafts, for example are known:[0004]The patent of Russia No 1808762, issue 15 Apr. 1993, bul. No 14;[0005]The patent of the USSR No 1828444, cl. B 64 B 1 / 00 issue 15 Jul. 1993, b...

Claims

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Application Information

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Patent Type & Authority Patents(United States)
IPC IPC(8): B64B1/20B64B1/26A62B99/00
CPCA62B5/00A62C29/00B64B1/36B64B1/20B64B2201/00
Inventor KHAKIMOV, BORIS V.CHERNIKOV, ALEXANDR N.DEMIDOV, GERMAN V.KHAMITOV, RUSTEM Z.
Owner KHAKIMOV BORIS V
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